View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 59588U 24077B 24313.09971227 .00046217 00000-0 49970-1 0 9995
2 59588 97.4975 348.3167 0038703 183.5302 176.5584 13.72501768 27097
Epoch (UTC): | 08 November 2024 02:23:35 |
Eccentricity: | 0.0038703 |
inclination: | 97.4975° |
perigee height: | 962 km |
apogee height: | 1019 km |
right ascension of ascending node: | 348.3167° |
argument of perigee: | 183.5302° |
revolutions per day: | 13.72501768 |
mean anomaly at epoch: | 176.5584° |
orbit number at epoch: | 2709 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|